WO2014044963A3 - Method for manufacturing composite parts and manufacturing equipment implementing such a method - Google Patents

Method for manufacturing composite parts and manufacturing equipment implementing such a method Download PDF

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Publication number
WO2014044963A3
WO2014044963A3 PCT/FR2013/052133 FR2013052133W WO2014044963A3 WO 2014044963 A3 WO2014044963 A3 WO 2014044963A3 FR 2013052133 W FR2013052133 W FR 2013052133W WO 2014044963 A3 WO2014044963 A3 WO 2014044963A3
Authority
WO
WIPO (PCT)
Prior art keywords
preform
manufacturing
mandrel
fabric
composite parts
Prior art date
Application number
PCT/FR2013/052133
Other languages
French (fr)
Other versions
WO2014044963A2 (en
Inventor
Bertrand Desjoyeaux
Original Assignee
Aircelle
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Aircelle filed Critical Aircelle
Priority to CN201380048497.8A priority Critical patent/CN104837608A/en
Priority to CA2881118A priority patent/CA2881118A1/en
Priority to BR112015003567A priority patent/BR112015003567A2/en
Priority to EP13779249.5A priority patent/EP2897784A2/en
Priority to RU2015113957A priority patent/RU2015113957A/en
Publication of WO2014044963A2 publication Critical patent/WO2014044963A2/en
Publication of WO2014044963A3 publication Critical patent/WO2014044963A3/en
Priority to US14/638,386 priority patent/US20150174833A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
    • B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • B29C70/222—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00—Making preforms
    • B29B11/14—Making preforms characterised by structure or composition
    • B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C67/00—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
    • B29C67/0014—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00 for shaping tubes or blown tubular films
    • B29C67/0018—Turning tubes inside out
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/25—Solid
    • B29K2105/253—Preform
    • B29K2105/258—Tubular
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2023/00—Tubular articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/772—Articles characterised by their shape and not otherwise provided for

Abstract

The present invention relates to a method for manufacturing composite parts and to manufacturing equipment. The invention is useful in the field of aircraft construction. During a first phase, the part is designed, the geometry is computed, and the fabric architecture of the fabric preform and a mandrel for forming the first state of the preform are calculated. During a second phase, the preform fabric (21) and the mandrel (20) are produced. During a third phase, the mandrel is wrapped with the fabric, the preform is extracted from the mandrel thereof in order to collapse (R) a portion (29b") of the preform, and the preform is impregnated in order to obtain the desired part.
PCT/FR2013/052133 2012-09-18 2013-09-17 Method for manufacturing composite parts, manufacturing equipment implementing such a method, and resulting composite parts WO2014044963A2 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CN201380048497.8A CN104837608A (en) 2012-09-18 2013-09-17 Method for manufacturing composite parts and manufacturing equipment implementing such method
CA2881118A CA2881118A1 (en) 2012-09-18 2013-09-17 Method for manufacturing composite parts and manufacturing equipment implementing such a method
BR112015003567A BR112015003567A2 (en) 2012-09-18 2013-09-17 METHOD FOR MANUFACTURING COMPOSITE MATERIAL PARTS WITH PREFORMS OBTAINED BY CONTOUR WEAVING AND INSTALLATION TO MANUFACTURE THEM
EP13779249.5A EP2897784A2 (en) 2012-09-18 2013-09-17 Method for manufacturing composite parts and manufacturing equipment implementing such a method
RU2015113957A RU2015113957A (en) 2012-09-18 2013-09-17 METHOD FOR PRODUCING COMPONENTS FROM COMPOSITE MATERIAL, INSTALLATION USING THIS METHOD, AND COMPONENT MATERIALS PRODUCED BY THIS METHOD
US14/638,386 US20150174833A1 (en) 2012-09-18 2015-03-04 Method for manufacturing composite parts, manufacturing facility implementing such a method, and composite parts manufactured thereby

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1258720A FR2995557A1 (en) 2012-09-18 2012-09-18 METHOD FOR MANUFACTURING COMPOSITE PARTS, MANUFACTURING PLANT USING SUCH A METHOD, AND COMPOSITE PARTS THUS MANUFACTURED
FR1258720 2012-09-18

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US14/638,386 Continuation US20150174833A1 (en) 2012-09-18 2015-03-04 Method for manufacturing composite parts, manufacturing facility implementing such a method, and composite parts manufactured thereby

Publications (2)

Publication Number Publication Date
WO2014044963A2 WO2014044963A2 (en) 2014-03-27
WO2014044963A3 true WO2014044963A3 (en) 2014-05-08

Family

ID=47295003

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2013/052133 WO2014044963A2 (en) 2012-09-18 2013-09-17 Method for manufacturing composite parts, manufacturing equipment implementing such a method, and resulting composite parts

Country Status (8)

Country Link
US (1) US20150174833A1 (en)
EP (1) EP2897784A2 (en)
CN (1) CN104837608A (en)
BR (1) BR112015003567A2 (en)
CA (1) CA2881118A1 (en)
FR (1) FR2995557A1 (en)
RU (1) RU2015113957A (en)
WO (1) WO2014044963A2 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3018286B1 (en) * 2014-03-10 2016-05-27 Aircelle Sa WOVEN PREFORM FOR REALIZING A CIRCUMFERENTIAL OR TORIC REINFORCEMENT WITH A SECTION IN OMEGA
DE102015205934B3 (en) * 2015-04-01 2016-09-22 Airbus Operations Gmbh Pressure bulkhead and method for producing a pressure bulkhead
FR3048435B1 (en) * 2016-03-02 2018-04-06 Safran Aircraft Engines INSTALLATION AND METHOD FOR MANUFACTURING FIBROUS BAND-SHAPED TEXTURE HAVING IN THE CROSS-SECTIONAL SECTION AN EVOLVING PROFILE
FR3053623B1 (en) * 2016-07-06 2018-08-17 Safran Nacelles METHOD FOR MANUFACTURING A PREFORM FOR COMPOSITE MATERIALS
FR3062659B1 (en) * 2017-02-03 2019-03-22 Safran Aircraft Engines CALL FOR PREFORM IN A JACQUARD-TYPE WEAVING
DE102017208182A1 (en) * 2017-05-16 2018-11-22 Bayerische Motoren Werke Aktiengesellschaft Method for defining a geometric shape of a core component for a fiber-reinforced braided component, core component for a fiber-reinforced braided component and fiber-reinforced braided component
FR3071765B1 (en) 2017-10-03 2020-11-20 Safran Ceram COMPOSITE MATERIAL REALIZATION OF A FLOW MIXER LOBE STRUCTURE
FR3085126B1 (en) * 2018-08-27 2020-09-11 Safran Nacelles METHOD OF MANUFACTURING A COMPOSITE PREFORM FOR THE MANUFACTURE OF A COMPOSITE PANEL WITH DOUBLE CURVED GEOMETRY
FR3098225B1 (en) * 2019-07-03 2021-07-16 3Ditex DEVICE FOR MAKING A PREFORM IN 3D, PROCESS FOR MAKING A 3D WITH THIS DEVICE, PREFORMING IN 3D THUS OBTAINED
CN114248463A (en) * 2020-09-21 2022-03-29 江苏金风科技有限公司 Fiber fabric, jig thereof and manufacturing method thereof
FR3116466B1 (en) * 2020-11-25 2022-11-25 Safran Ceram Fiber preform of a turbomachinery blade airfoil
CN113085222B (en) * 2021-04-01 2023-03-21 湖北航泰科技有限公司 Composite material reinforcement and forming process method
DE102021109699A1 (en) * 2021-04-16 2022-10-20 Airbus Operations Gmbh Process for producing composite components with a non-developable surface
FR3129392B1 (en) * 2021-11-22 2023-11-17 Safran Ceram Process for obtaining a part made of composite material with a ceramic matrix.

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Publication number Priority date Publication date Assignee Title
US4534813A (en) * 1982-07-26 1985-08-13 Mcdonnell Douglas Corporation Compound curve-flat pattern process
EP1584452A2 (en) * 2004-04-08 2005-10-12 Grundfos a/s Process for forming a formstable hollowlike element having a bottom and use of such an element.
DE102005041940A1 (en) * 2005-08-30 2007-03-01 Technische Universität Dresden Wheel rim for vehicle, has twisted tube formed with unit for fixing textile reinforcement and supporting core, where entire geometry of rim is plunged by twisted tube in uninterruptable manner
WO2009035344A2 (en) * 2007-09-11 2009-03-19 Lingk & Sturzebecher Leichtbau Gmbh End-fittings for composite tubes, method for joining fittings to the ends of composite tubes and composite tubes incorporating end-fittings
US20090098337A1 (en) * 2007-10-16 2009-04-16 Ming Xie Substantially cylindrical composite articles and fan casings
WO2012059886A1 (en) * 2010-11-03 2012-05-10 University Of Ottawa Novel composite parts, methods and apparatus for manufacturing the same

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CN1056800C (en) * 1994-12-20 2000-09-27 波音公司 Hand assisted lamination system
FR2935990B1 (en) * 2008-09-17 2011-05-13 Aircelle Sa PROCESS FOR MANUFACTURING A PIECE OF METALLIC MATRIX COMPOSITE MATERIAL
DE102010053635B4 (en) * 2010-12-07 2017-05-11 Hero Gmbh Process for producing a fiber composite product

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4534813A (en) * 1982-07-26 1985-08-13 Mcdonnell Douglas Corporation Compound curve-flat pattern process
EP1584452A2 (en) * 2004-04-08 2005-10-12 Grundfos a/s Process for forming a formstable hollowlike element having a bottom and use of such an element.
DE102005041940A1 (en) * 2005-08-30 2007-03-01 Technische Universität Dresden Wheel rim for vehicle, has twisted tube formed with unit for fixing textile reinforcement and supporting core, where entire geometry of rim is plunged by twisted tube in uninterruptable manner
WO2009035344A2 (en) * 2007-09-11 2009-03-19 Lingk & Sturzebecher Leichtbau Gmbh End-fittings for composite tubes, method for joining fittings to the ends of composite tubes and composite tubes incorporating end-fittings
US20090098337A1 (en) * 2007-10-16 2009-04-16 Ming Xie Substantially cylindrical composite articles and fan casings
WO2012059886A1 (en) * 2010-11-03 2012-05-10 University Of Ottawa Novel composite parts, methods and apparatus for manufacturing the same

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Also Published As

Publication number Publication date
WO2014044963A2 (en) 2014-03-27
RU2015113957A (en) 2016-11-10
CN104837608A (en) 2015-08-12
FR2995557A1 (en) 2014-03-21
BR112015003567A2 (en) 2017-08-15
EP2897784A2 (en) 2015-07-29
US20150174833A1 (en) 2015-06-25
CA2881118A1 (en) 2014-03-27

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